ROTOR ASSEMBLY HAVING LIQUID COOLING

• US 20140175916A1
• Filed: 12/20/2012
• Published: 06/26/2014
• Est. Priority Date: 12/20/2012
• Status: Abandoned Application

• Current Assignee: Remy Technologies LLC (BorgWarner Incorporated)
• Original Assignee: Remy Technologies LLC (BorgWarner Incorporated)
• Inventors: Chamberlin, Bradley D., Hamer, Colin
• Application Number:
  US13/721,856
• Publication Number:
  US 20140175916A1
• Time in Patent Office: Days
• US Class Current: 310/54
• CPC Class Codes: H02K 1/2766 having a flux concentration effect
• CPC Class Codes: H02K 1/32 with channels or ducts for flow of cooling medium
• CPC Class Codes: H02K 9/19 for machines with closed casing and closed-circuit cooling using a liquid cooling medium, e.g. oil

Abstract

A liquid-cooled rotor assembly for a rotary electric machine, including a shaft provided with a fluid passageway receivable of a liquid coolant, and a substantially cylindrical rotor core rotatable in unison with the shaft. The rotor core is provided with a plurality of passages each terminating at a void in a rotor core axial end. Permanent magnets are disposed in rotor core passages, a gap is defined between each magnet and its respective rotor core passage. The shaft fluid passageway is in fluid communication with the rotor core end voids through the gaps, whereby the rotor core and the magnets are convectively cooled by liquid coolant receivable by the shaft fluid passageway and delivered to a rotor core end through the rotor core passages. Also, a method for liquid cooling a rotor assembly.

Claims

1. A liquid-cooled rotor assembly for a rotary electric machine, comprising:

a rotatively-supportable shaft defining a central axis about which said rotor assembly is rotatable, said shaft provided with a fluid passageway receivable of a liquid coolant;

a substantially cylindrical rotor core disposed about said central axis and rotatable in unison with said shaft, said rotor core having axially opposite ends, said rotor core provided with a plurality of passages, each said rotor core passage terminating at a void in a said rotor core axial end; and

a plurality of permanent magnets distributed about said central axis, each magnet of said plurality of magnets disposed in a said rotor core passage, a gap defined between said each magnet and its respective said rotor core passage, said shaft fluid passageway in fluid communication with said rotor core end voids through said gaps, whereby said rotor core and said plurality of magnets are convectively cooled by liquid coolant receivable by said shaft fluid passageway and delivered to a said rotor core end through said rotor core passages.

2. The rotor assembly of claim 1, wherein said shaft fluid passageway has a generally axially-extending first leg and at least one generally radially-extending second leg, said first leg and a said rotor core end void in fluid communication through said second leg, liquid coolant receivable into said shaft fluid passageway first leg urged from said shaft fluid passageway through said shaft fluid passageway second leg and towards said rotor core passage by rotation of said rotor assembly about said central axis.

3. The rotor assembly of claim 1, further comprising:

a hub disposed radially between and interconnecting said shaft and said rotor core, said hub provided with a fluid duct through which said shaft fluid passageway and a said rotor core passage are fluidly connected.

4. The rotor assembly of claim 3, wherein said hub fluid duct has a generally radially-extending portion along which liquid coolant receivable into said hub fluid duct is urged towards said rotor core by rotation of said rotor assembly about said central axis.

5. The rotor assembly of claim 3, wherein one of said shaft and said hub is provided with a circumferentially-extending groove through which said hub fluid duct and said shaft fluid passageway are fluidly connected.

6. The rotor assembly of claim 1, wherein said plurality of rotor core passages is distributed about said central axis.

7. The rotor assembly of claim 1, wherein each magnet of said plurality of magnets is elongate and entirely surrounded about its length by its respective said rotor core passage.

8. The rotor assembly of claim 1, wherein a said rotor passage includes a generally radially-extending trunk and a generally axially-extending branch, a said magnet disposed in a said rotor core branch.

9. The rotor assembly of claim 8, wherein relative to a said rotor core passage, said trunk and said void are fluidly connected with each other through said branch.

10. The rotor assembly of claim 8, wherein a multiplicity of said rotor core passages includes a multiplicity of said branches and a common said trunk to which said multiplicity of branches is fluidly connected.

11. The rotor assembly of claim 8, wherein a said rotor core passage includes a multiplicity of said trunks and a common said branch with which said multiplicity of trunks is fluidly connected.

12. The rotor assembly of claim 8, wherein said rotor core comprises an axially-stacked plurality of carrier laminae each mutually adjacent to another of said plurality, and at least one distribution lamina axially adjacent said plurality of carrier laminae, said plurality of carrier laminae defining a plurality of said branches, a plurality of said trunks defined by said at least one distribution lamina and at least one said carrier lamina.

13. The rotor assembly of claim 1, further comprising a manifold disposed about said central axis and sealed to a said rotor core end, said manifold defining a collection space into which liquid coolant is receivable from said rotor core end voids, said shaft fluid passageway and said collection space in fluid communication with each other through said plurality of rotor core passages.

14. The rotor assembly of claim 13, wherein a said rotor core end void defines one of a plurality of liquid coolant inlets to said collection space, said manifold having at least one outlet from which liquid coolant is expelled from said collection space.

15. The rotor assembly of claim 14, wherein the total size of said at least one manifold outlet is smaller than the total size of said plurality of inlets to said manifold, whereby said manifold may be pressurized with liquid coolant receivable therein.

16. The rotor assembly of claim 14, wherein each said manifold outlet is a pressure controlled orifice, whereby spaces for liquid coolant in said rotor assembly may remain full of liquid coolant during rotation of said rotor assembly.

17. The rotor assembly of claim 13, wherein said manifold defines a balance ring rotatable in unison with said shaft.

18. A rotary electric machine comprising:

a rotor assembly according to claim 1; and

a stator assembly;

wherein said rotor assembly is surrounded by and rotatable relative to said stator assembly.

19. A method for liquid cooling a rotor assembly in a rotary electric machine, comprising:

receiving liquid coolant into a fluid passageway located in a shaft of the rotor assembly;

rotating a substantially cylindrical rotor core of the rotor assembly and the shaft in unison about an axis;

urging liquid coolant radially outwardly of the shaft and into an internal passage extending through the rotor core;

directing liquid coolant received into the rotor core passage, through a gap defined by a permanent magnet disposed in the rotor core passage and an internal wall of the rotor core passage surrounding the magnet, and out of the rotor core; and

convectively cooling the rotor core and the permanent magnet with liquid coolant directed through the gap.

20. The method of claim 19, further comprising providing a hub radially between the shaft and the rotor core, and fluidly connecting the shaft fluid passageway and the rotor core passage through a fluid duct in the hub.